APA (7th ed.) Citation

Takahashi, H., Munakata, T., & Sato, S. (2018, February). Thrust Augmentation by Airframe-Integrated Linear-Spike Nozzle Concept for High-Speed Aircraft. Aerospace.

Chicago Style (17th ed.) Citation

Takahashi, Hidemi, Toshihiko Munakata, and Shigeru Sato. "Thrust Augmentation by Airframe-Integrated Linear-Spike Nozzle Concept for High-Speed Aircraft." Aerospace Feb. 2018.

MLA (9th ed.) Citation

Takahashi, Hidemi, et al. "Thrust Augmentation by Airframe-Integrated Linear-Spike Nozzle Concept for High-Speed Aircraft." Aerospace, Feb. 2018.